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Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications
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This open-access book reports on both experimental and numerical findings from the H2020-funded project TEAMAero (Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications). It covers novel contributions on improving the fundamental understanding of the physics of shock wave boundary layer interaction, developments in flow control for mitigation of shock effects, and advanced numerical methods for predicting those effects. All in all, this book offers a timely snapshot of research and developments in numerical methods for flow analysis and control, with a special emphasis on high-speed flows. It offers extensive information to both researchers and professionals.
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- 10 - pdf (CC BY) at OAPEN Library.
Keywords
- High-Fidelity CFD
- Reduced-Order Modeling
- Supersonic Boundary-Layer Control
- thema EDItEUR::P Mathematics and Science::PH Physics::PHU Mathematical physics
- Transitional Shock Wave Boundary Layer Interaction
- Transonic Interaction and Morphing
- Unsteady Separated Flows
- Unsteady Wall-Pressure Measurements
Links
DOI: 10.1007/978-3-031-86605-0Editions